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CA2687437A1 - Element structural d'aeronef situe a l'interface entre une aile et le fuselage - Google Patents

Element structural d'aeronef situe a l'interface entre une aile et le fuselage Download PDF

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Publication number
CA2687437A1
CA2687437A1 CA002687437A CA2687437A CA2687437A1 CA 2687437 A1 CA2687437 A1 CA 2687437A1 CA 002687437 A CA002687437 A CA 002687437A CA 2687437 A CA2687437 A CA 2687437A CA 2687437 A1 CA2687437 A1 CA 2687437A1
Authority
CA
Canada
Prior art keywords
fin
web
element according
profiled
fins
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002687437A
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English (en)
Other versions
CA2687437C (fr
Inventor
Anne-Laure Lafly
Franck Batalla
Henri Leman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2687437A1 publication Critical patent/CA2687437A1/fr
Application granted granted Critical
Publication of CA2687437C publication Critical patent/CA2687437C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
    • B23K20/1225—Particular aspects of welding with a non-consumable tool
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Braking Arrangements (AREA)
  • Connection Of Plates (AREA)
CA2687437A 2007-05-23 2008-05-13 Element structural d'aeronef situe a l'interface entre une aile et le fuselage Expired - Fee Related CA2687437C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0755228A FR2916417B1 (fr) 2007-05-23 2007-05-23 Element structural d'aeronef situe a l'interface entre une aile et le fuselage
FR0755228 2007-05-23
PCT/FR2008/000662 WO2008152248A2 (fr) 2007-05-23 2008-05-13 Élément structural d'aéronef situé à l'interface entre une aile et le fuselage

Publications (2)

Publication Number Publication Date
CA2687437A1 true CA2687437A1 (fr) 2008-12-18
CA2687437C CA2687437C (fr) 2015-12-08

Family

ID=38754582

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2687437A Expired - Fee Related CA2687437C (fr) 2007-05-23 2008-05-13 Element structural d'aeronef situe a l'interface entre une aile et le fuselage

Country Status (10)

Country Link
US (1) US8720823B2 (fr)
EP (1) EP2178746B1 (fr)
JP (1) JP5373773B2 (fr)
KR (1) KR20100068231A (fr)
CN (1) CN101687541B (fr)
BR (1) BRPI0810287A2 (fr)
CA (1) CA2687437C (fr)
FR (1) FR2916417B1 (fr)
RU (1) RU2478519C2 (fr)
WO (1) WO2008152248A2 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2916417B1 (fr) * 2007-05-23 2009-07-24 Airbus France Sas Element structural d'aeronef situe a l'interface entre une aile et le fuselage
ES2351823B1 (es) 2007-12-21 2011-12-05 Airbus Operations, S.L. Estructura sustentadora para aeronaves.
ES2392617B1 (es) * 2010-01-15 2013-11-21 Airbus Operations S.L. Disposición de unión de los cajones laterales de un estabilizador horizontal de cola con un cajón central tubular y procedimiento de fabricación de dicho cajón.
ES2372849B1 (es) * 2010-03-25 2012-12-13 Airbus Operations, S.L. Estructura de unión de cajones de torsión en una aeronave mediante un herraje triforme de materiales compuestos no metálicos.
GB201009922D0 (en) * 2010-06-14 2010-07-21 Airbus Uk Ltd Aircraft wing box joint
FR2972997B1 (fr) 2011-03-25 2013-05-10 Airbus Operations Sas Raccordement d'un fuselage a une voilure d'aeronef
GB201110973D0 (en) * 2011-06-28 2011-08-10 Airbus Operations Ltd Bracket
FR2991228B1 (fr) 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
US10118686B2 (en) * 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
GB201217801D0 (en) 2012-10-05 2012-11-14 Airbus Operations Ltd An aircraft structure
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
FR3040684A1 (fr) * 2015-09-04 2017-03-10 Airbus Operations Sas Nervure simplifiee pour caisson central de voilure d'aeronef.
RU2621925C1 (ru) * 2016-01-28 2017-06-08 Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") Стык консоли крыла с центропланом самолета
US10479474B2 (en) 2016-07-14 2019-11-19 The Boeing Company Friction stir welded wingtip torque box
FR3074143A1 (fr) * 2017-11-29 2019-05-31 Airbus Operations Nervure de jonction voilure-caisson de voilure pour aeronef et procede de fabrication d'un aeronef au moyen d'une telle nervure
US11358703B2 (en) * 2020-03-18 2022-06-14 The Boeing Company Monolithic wing to side body upper chord assembly for aircraft

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2116953A (en) * 1934-09-07 1938-05-10 Sambraus Adolf Airplane structure
US2210163A (en) * 1938-03-07 1940-08-06 Ryan Aeronautical Co Airplane wing and wing spar
US2318909A (en) * 1940-10-02 1943-05-11 Bell Aircraft Corp Wing construction
US2367750A (en) * 1941-01-17 1945-01-23 Central Aircraft Corp Aircraft construction
US2396625A (en) * 1941-03-26 1946-03-12 Budd Edward G Mfg Co Aircraft structure
US2618448A (en) * 1941-12-12 1952-11-18 Robert Roger Aime Structure for airplane wings
US2393081A (en) * 1943-06-28 1946-01-15 Budd Edward G Mfg Co Joint construction
FR1523404A (fr) * 1967-03-22 1968-05-03 Sud Aviation Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne
US5297760A (en) * 1992-08-21 1994-03-29 Mcdonnell Douglas Corporation Aircraft skin lap splice
CN1204288A (zh) * 1995-12-15 1999-01-06 波音公司 多用途通用机体基本结构的飞机
US7509740B2 (en) * 2001-11-13 2009-03-31 The Boeing Company Method of manufacturing a wing
CN1089049C (zh) * 1996-03-22 2002-08-14 波音公司 飞机翼梁,装配飞机翼梁的方法和翼弦定位工具
GB9713209D0 (en) * 1997-06-20 1997-08-27 British Aerospace Friction welding metal components
US6116539A (en) * 1999-03-19 2000-09-12 Williams International Co. L.L.C. Aeroelastically stable forward swept wing
US6398883B1 (en) * 2000-06-07 2002-06-04 The Boeing Company Friction stir grain refinement of structural members
US20030226935A1 (en) * 2001-11-02 2003-12-11 Garratt Matthew D. Structural members having improved resistance to fatigue crack growth
GB2409443A (en) * 2003-12-23 2005-06-29 Airbus Uk Ltd Rib for an aircraft and the manufacture thereof
EP1799391B8 (fr) * 2004-09-14 2009-08-12 Alcan Rhenalu Element de structure soude comprenant au moins deux parties en alliages d'aluminium presentant un etat metallurgique different, procede de fabrication d'un tel element
CA2529108C (fr) * 2004-12-07 2012-10-30 Airbus Deutschland Gmbh Aile d'avion, methode de fabrication et procede de soudage applicable a un longeron d'aile
FR2894859A1 (fr) * 2005-12-16 2007-06-22 Alcan Rhenalu Sa Longeron de voilure soude et son procede de fabrication
GB0606079D0 (en) * 2006-03-27 2006-05-03 Airbus Uk Ltd Aircraft component
FR2916417B1 (fr) * 2007-05-23 2009-07-24 Airbus France Sas Element structural d'aeronef situe a l'interface entre une aile et le fuselage
CN102112263B (zh) * 2008-07-07 2014-07-16 肯联铝业瑞士有限公司 一种接合铝和钛的熔焊方法

Also Published As

Publication number Publication date
CN101687541B (zh) 2013-02-13
WO2008152248A3 (fr) 2009-02-12
WO2008152248A8 (fr) 2010-04-22
FR2916417A1 (fr) 2008-11-28
US8720823B2 (en) 2014-05-13
WO2008152248A2 (fr) 2008-12-18
US20100170986A1 (en) 2010-07-08
RU2478519C2 (ru) 2013-04-10
CA2687437C (fr) 2015-12-08
JP2010527832A (ja) 2010-08-19
KR20100068231A (ko) 2010-06-22
BRPI0810287A2 (pt) 2014-12-30
CN101687541A (zh) 2010-03-31
EP2178746B1 (fr) 2012-09-05
FR2916417B1 (fr) 2009-07-24
RU2009147734A (ru) 2011-06-27
JP5373773B2 (ja) 2013-12-18
EP2178746A2 (fr) 2010-04-28

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